An integrated approach is proposed to modeling and control of lightly damped systems such as flexible structures using frequency loopshaping in ℓ∞. Normalized coprime factors of the shaped plant model are identified with quantification of the modeling error in ℓ∞ norm. Feedback controllers are synthesized to stabilize the true but unknown plant albeit the nominal feedback system, consisting of the identified model and the feedback controller, may not be stable. A complete design procedure is presented that integrates modeling and control in frequency domain. It is shown that as the ℓ∞ norm of the modeling error measured in normalized coprime factors of the system is reduced, the existence of stabilizing feedback controllers for the true unk...
Quantitative feedback theory can be used to achieve frequency-domain specifications for the tip of a...
This paper presents a robust noniterative algorithm for the design of controllers of a given structu...
The major components of a design and operational flight strategy for flexible structure control syst...
The determination of the structural modes which are important for control is a major issue in the fi...
Application of the normalised H∞ CG loop-shaping technique for design and simplification of damping ...
ABSTRACT: The combined system consisting of the baseline flexible structure modified by the system o...
In the modeling of flexible structures, there is generally uncertainty in both the frequencies and d...
A balanced approach to shaping the closed-loop properties of the dissipative controllers for flexibl...
A comparison is made between three partial differential equation models for a flexible beam with dif...
©1989 IEEE. Personal use of this material is permitted. However, permission to reprint/republish thi...
A comparison is made between three partial differential equation models for a flexible beam with dif...
The monograph covers the topic of vibration control for large scale flexible structures subject to b...
In the modeling of flexible structures, there is generally uncertainty in both the frequencies and d...
©1986 ASMESubmitted for presentation at the 1986 ASME Winter Annual Meeting.The authors have suggest...
An accurate multivariable transfer function model of an experimental structure is required for resea...
Quantitative feedback theory can be used to achieve frequency-domain specifications for the tip of a...
This paper presents a robust noniterative algorithm for the design of controllers of a given structu...
The major components of a design and operational flight strategy for flexible structure control syst...
The determination of the structural modes which are important for control is a major issue in the fi...
Application of the normalised H∞ CG loop-shaping technique for design and simplification of damping ...
ABSTRACT: The combined system consisting of the baseline flexible structure modified by the system o...
In the modeling of flexible structures, there is generally uncertainty in both the frequencies and d...
A balanced approach to shaping the closed-loop properties of the dissipative controllers for flexibl...
A comparison is made between three partial differential equation models for a flexible beam with dif...
©1989 IEEE. Personal use of this material is permitted. However, permission to reprint/republish thi...
A comparison is made between three partial differential equation models for a flexible beam with dif...
The monograph covers the topic of vibration control for large scale flexible structures subject to b...
In the modeling of flexible structures, there is generally uncertainty in both the frequencies and d...
©1986 ASMESubmitted for presentation at the 1986 ASME Winter Annual Meeting.The authors have suggest...
An accurate multivariable transfer function model of an experimental structure is required for resea...
Quantitative feedback theory can be used to achieve frequency-domain specifications for the tip of a...
This paper presents a robust noniterative algorithm for the design of controllers of a given structu...
The major components of a design and operational flight strategy for flexible structure control syst...